EP 3252271 B1 20210811 - BLADE ASSEMBLY, CORRESPONDING FAN SECTION AND GAS TURBINE ENGINE
Title (en)
BLADE ASSEMBLY, CORRESPONDING FAN SECTION AND GAS TURBINE ENGINE
Title (de)
SCHAUFELBAUSATZ, ZUGEHÖRIGE FANSTUFE UND GASTURBINENTRIEBWERK
Title (fr)
ENSEMBLE POUR AUBE, ÉTAGE DE SOUFFLANTE ET MOTEUR À TURBINE À GAZ ASSOCIÉS
Publication
Application
Priority
US 201615163933 A 20160525
Abstract (en)
[origin: EP3252271A1] A blade assembly (100;150) may be configured to rotate about an axis of a gas turbine engine (20). The blade assembly may include a blade (102) and a blade cover (200). A blade (102) may include a first surface (132) defining a perimeter of a cavity (130) in the blade (102). A first portion (136) of the perimeter (134) of the cavity (130) includes a lip (142). A blade cover (200) disposed over the cavity (130) in the blade (102), such that the cavity (130) is disposed between the blade (102) and the blade cover (200), and under the lip (142), such that blade cover (200) is between a portion of the blade (102) and the cavity (130).
IPC 8 full level
CPC (source: EP US)
F01D 5/147 (2013.01 - EP US); F01D 5/16 (2013.01 - EP US); F05D 2220/36 (2013.01 - EP US); F05D 2260/36 (2013.01 - EP US); Y02T 50/60 (2013.01 - EP US)
Citation (examination)
- EP 1983160 A2 20081022 - UNITED TECHNOLOGIES CORP [US]
- FR 2139741 A1 19730112 - SNECMA
- WO 2015095205 A1 20150625 - UNITED TECHNOLOGIES CORP [US]
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
EP 3252271 A1 20171206; EP 3252271 B1 20210811; US 10280759 B2 20190507; US 2017343007 A1 20171130
DOCDB simple family (application)
EP 17172938 A 20170525; US 201615163933 A 20160525